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Flying the Garmin G1000
Ed Williams CFII/ATP SMX-XX April 2008
An intro to glass panels
Primary Flight Display (PFD) Multi-Function Display (MFD)
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Garmins G1000 panel dominates
the newairplane market
Cessna 172, 182, T206Beech G36
Columbia 400Diamond DA40, DA42Mooney Ovation 20RTiger AG-5BVLJs etc
The promise is greater functionality at lower cost. Better maintainability and reliability than analog instrumentation? Not just data, but information.
Diamond DA42 twinstar
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The G1000 is a integrated
system of communicatingmodules.
Service is primarily swappingLRUs and repairing them in-
house or back at Garmin.
The various LRUs are commonto many different airframesfrom the C172 to VLJs.
Im familiar with the C172Sconfiguration, so Illconcentrate on that.
Its modular
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In the G1000 flight data are measured by remote sensors
and displayed on the PFD.
= +
GDC74A air data computer
Altitude
ROC
Solid state electronic pressure sensors replacemechanical instruments.
Sensor and display are separate.
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In addition we have an altitude bug and a 6-second trend vector.
Altitude bug
Altimeter setting
6 second trend
The altitude bug is notintegrated with theKAP140 autopilot. Ithas to be set
independently.
In theC172S/G1000/KAP140,there are threealtimeters to set!
Garmin has recentlyintroduced its ownintegrated autopilot.
GarminGFC700
A/P
Altitude bug
The altimeter is set with the
outer knob of the OBS courseselector on the RH bezel.
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The airspeed indicator is also replaced with a tape.
TAS is computedautomatically.Vr, Vx, Vy bugs can beadjusted from thedefaults.
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The AHRS will degrade into a reversionary mode if
external inputs are lost. It has some redundancy
Normal AHRSAHRS w/o magnetometer
The ball.
Rate ofturn(6 sec
trend)
Standardrate mark.
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The heading display incorporates an HSI for the
primary navaid (GPS, VOR or ILS).
We are intercepting the071bearing to RIS VORon a 042heading.
Inner knob sets
the OBS coursepointer. Pressinggives direct-to.
NAV1 active is 111.4 (RIS)Standby is 117.95.
Primary nav on the HSItoggled with the CDI
soft-key
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Here we show the whole Primary Flight Display
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Its all electrical except for three standby instruments
Airspeed, Attitude & Altimeter
Cessna 182
If a panel fails, the remaining panel can operate in reversionarymode.(Automatic or the red button.)
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In reversionary mode, the PFD display adds engine instrumentation.
Normally, engine data only shows on the MFD.
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In the C172/Garmin 1000 a standby battery can power the essential bus.
Essentialbus powers PFD, AHRS, engine/airframesensors, #1 Nav-Com and 1 GPS.
If the alternator fails, turning off the master switch andleaving the stand-by battery switch armedwill allow
you to preserve main battery capacity for later in theflight.
The standby battery has little or no power remainingonce the essential bus voltage drops to 20V.
(excerpted from the C172S manual)
From the starting checklist:
4. STBY BATT Switch TEST (hold for 20 sec, verify thegreen test lamp does not go out), then ARM (verify PFDcomes on)
checks the condition of the standby battery.
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The GPS interface will be familiar to Garmin 430/530 users.
FPL on the PFD
More extensive planning
options on the MFD page.
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Curiously, the direct/direct shortcut for activating a flight plan
leg is absent on the G1000.
You can still useactivate legvia themenukey, or onthe MFD only, usethe act-legsoft-key.
ECA-KSMX leg active
Soft key.
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The MAP page on the MFD shows the flight plan and position.
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The MFD map can display terrain, traffic, nexrad, lightning
with the necessary optional equipment installed
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The MFD is showing XM NEXRAD data.
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I highly recommend this book
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The King School is a good overview -- but is $249
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The Garmin simulators are faithful and essential
Harder to fly than the 430/530 simulators IMODual screens add realism.
FS X supposedly has a partial simulation.
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If youve not flown a glass panel, give it a try.
I found the instrument display intuitive easy to transition to.
Practice with the simulator was greatly rewarded.
The GPS is easy if you know the 430/530.
Keep looking out the window!!